公开(公告)号：US20120201689A1

公开(公告)日：2012-08-09

申请号：US13500573

申请日：2010-10-08

Applicant: Peter Fuglsang ,  Stefano Bove ,  Peter Grabau ,  V.v. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

Inventor： Peter Fuglsang ,  Stefano Bove ,  Peter Grabau ,  V.v. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

IPC: F03D1/06

CPC classification number: F03D1/0641 ,  F05B2240/121 ,  F05B2240/301 ,  F05B2260/30 ,  Y02E10/721

Abstract: A wind turbine blade (10) for a rotor of a wind turbine (2) is provided with a longitudinally extending flow guiding device (70, 170) attached to the profiled contour. The flow guiding device comprises: a base (90, 190) having a first longitudinal end (91, 191) nearest the root end (16) and a second longitudinal end (92, 192) nearest the tip end (14), a first side (93, 193) nearest the leading edge (18) and a second side (94, 194) nearest the trailing edge (20), as well as a first surface (95, 195) and a second surface (96, 196), the first surface of the base being attached to the profiled contour, and the second surface facing away from the profiled contour. A longitudinally extending substantially plate-shaped element (97, 197) protrudes from the second surface (96, 196) of the base (90, 190).

Abstract translation: 用于风力涡轮机（2）的转子的风力涡轮机叶片（10）设置有附接到成型轮廓的纵向延伸的流动引导装置（70,170）。 流动引导装置包括：具有最靠近根端（16）的第一纵向端（91,191）和最靠近末端（14）的第二纵向端（92,192）的底座（90,190），第一 最靠近前缘（18）的第二侧（93,193）和最靠近后缘（20）的第二侧（94,194）以及第一表面（95,195）和第二表面（96,196） 底座的第一表面附着在成型轮廓上，第二表面背离轮廓。 从基座（90,190）的第二表面（96,196）突出的纵向延伸的基本上板状的元件（97,197）。

公开(公告)号：US20120195764A1

公开(公告)日：2012-08-02

申请号：US13500673

申请日：2010-10-08

Applicant: Peter Fuglsang ,  Stefano Bove ,  V.V. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

Inventor： Peter Fuglsang ,  Stefano Bove ,  V.V. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

IPC: F03D11/02

CPC classification number: F03D1/0641 ,  F05B2240/121 ,  F05B2240/301 ,  Y02E10/721

Abstract: A wind turbine blade with a plurality of flow guiding device parts attached to a profiled contour on a pressure side of the blade is described. The longitudinally extending flow guiding device parts are grouped together to form a first flow guiding device group in the transition region of the blade.

Abstract translation: 描述了具有附接到叶片的压力侧上的轮廓轮廓的多个导流装置部件的风力涡轮机叶片。 纵向延伸的导流装置部件分组在一起以在叶片的过渡区域中形成第一导流装置组。

公开(公告)号：US20120070281A1

公开(公告)日：2012-03-22

申请号：US13320928

申请日：2010-05-18

Applicant: Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

Inventor： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

IPC: F03D7/02

CPC classification number: F03D1/0641 ,  F03D7/0224 ,  F03D7/0232 ,  F05B2240/301 ,  F05B2240/32 ,  Y02E10/721 ,  Y02E10/723

Abstract: A wind turbine is operated with a blade in which a transition region is provided between a root region with a substantially circular or elliptical profile closest to a hub and an airfoil region with a lift generating profile furthest away from the hub. The transition region has a base part with an inherent non-ideal aerodynamic design so that a substantial longitudinal part of the base part without flow altering devices at a design point deviates from a target axial induction factor. A pitch of the blade and a rotational speed are adjusted to meet the target axial induction factor of the second longitudinal segment, and flow altering devices are provided so as to meet the target axial induction factor of the first longitudinal segment.

Abstract translation: 风力涡轮机用叶片操作，其中过渡区域设置在最靠近轮毂的基本圆形或椭圆形轮廓的根部区域和具有离轮毂最远的提升产生轮廓的翼型区域之间。 过渡区域具有固有的非理想空气动力学设计的基部，使得在设计点处没有流动改变装置的基部的基本纵向部分偏离目标轴向感应系数。 调整叶片的间距和转速以满足第二纵向段的目标轴向感应系数，并且提供换流装置以满足第一纵向段的目标轴向感应系数。

公开(公告)号：US20100209258A1

公开(公告)日：2010-08-19

申请号：US12733403

申请日：2008-08-29

Applicant: Peter Fuglsang ,  Stefano Bove

Inventor： Peter Fuglsang ,  Stefano Bove

IPC: F03D1/06 ,  F03D7/02

CPC classification number: F03D1/0633 ,  F03D1/0641 ,  F03D7/0228 ,  F03D7/0232 ,  F03D7/0252 ,  F03D7/0256 ,  F05B2240/32 ,  F05B2260/90 ,  F05B2270/20 ,  Y02E10/721 ,  Y02E10/723

Abstract: A blade for a rotor of a wind turbine has a substantially horizontal rotor shaft, the rotor including a hub, from which the blade extends substantially in a radial direction when mounted to the hub. The blade includes a profiled contour including a leading edge and a trailing edge as well as a pressure side and a suction side, the profiled contour when being impacted by an incident airflow generating a lift. The profiled contour is divided into a root region with a substantially circular profile closest to the hub, an airfoil region with a lift generating profile furthest away from the hub, and a transition region between the root region and the airfoil region. The profile of the transition region gradually changes in the radial direction from the circular profile of the root region to the lift generating profile of the airfoil region. The suction side comprises at least a first zone, which extends substantially in the direction of the incident airflow, and which is positioned in a zone of a cross-flow. The first zone includes a first barrier generating means adapted to generating a barrier of airflow, which extends essentially in the direction of the incident airflow, the barrier of airflow being of sufficient strength and length so as to effectively reduce the cross-flow.

Abstract translation: 用于风力涡轮机的转子的叶片具有基本上水平的转子轴，转子包括轮毂，当安装到轮毂时，叶片从该轮毂基本上沿径向方向延伸。 叶片包括外形轮廓，其包括前缘和后缘以及压力侧和吸力侧，当受到产生升力的入射气流的冲击时，轮廓轮廓。 成型轮廓被分成具有最靠近轮毂的基本上圆形轮廓的根部区域，具有离轮毂最远的升力产生轮廓的翼型区域以及根部区域和翼型区域之间的过渡区域。 过渡区域的轮廓在径向方向上从根部区域的圆形轮廓到翼型区域的升力产生轮廓逐渐变化。 吸入侧包括至少第一区域，其基本上沿着入射气流的方向延伸，并且位于交叉流动的区域中。 第一区域包括适于产生基本上沿着入射气流的方向延伸的气流障碍物的第一障碍物产生装置，气流阻挡层具有足够的强度和长度，以便有效地减少交叉流动。

公开(公告)号：US10267289B2

公开(公告)日：2019-04-23

申请号：US13500868

申请日：2010-10-08

Applicant: Peter Fuglsang ,  Stefano Bove ,  Peter Grabau ,  V. V. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

Inventor： Peter Fuglsang ,  Stefano Bove ,  Peter Grabau ,  V. V. Subrahmanyam ,  Brian Lund ,  Lars E. Jensen ,  Sreeram Kottumuklu Radhakrishnan

IPC: F03D1/06

Abstract: A wind turbine blade with a flow guiding device attached to a profiled contour on a pressure side of the blade is described. The flow guiding device has a front surface facing toward an oncoming airflow and comprises at least a first portion, which is angled towards the oncoming airflow and a leading edge of the wind turbine blade.

公开(公告)号：US09611833B2

公开(公告)日：2017-04-04

申请号：US13810049

申请日：2010-07-16

Applicant: Jesper Madsen ,  Christian Frank Andersen ,  Peter Fuglsang

Inventor： Jesper Madsen ,  Christian Frank Andersen ,  Peter Fuglsang

IPC: F03D1/06

CPC classification number: F03D1/0633 ,  F03D1/0641 ,  F05B2240/301 ,  F05B2250/62 ,  F05B2250/71 ,  Y02E10/721

Abstract: A blade (10) for a rotor of a wind turbine having a profiled contour divided into: a root region (30), an airfoil region (34), and a transition region (32) between the root region (30) and the airfoil region (34). A shoulder (40) is located at the boundary between the transition region (32) and the airfoil region (34). The blade's profiled contour comprises a local relative thickness defined as the local ratio between a maximum profile thickness (t) and the chord length (c). The ratio between the shoulder width (W) and the blade length (L) being less than or equal to 0.075, and the relative thickness (t/c) in a blade length interval of 0-0.8 L is at least 22%.

公开(公告)号：US08888453B2

公开(公告)日：2014-11-18

申请号：US13320946

申请日：2010-05-18

Applicant: Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

Inventor： Peter Fuglsang ,  Stefano Bove ,  Lars Fuglsang

IPC: F03D11/00 ,  F03D1/06

CPC classification number: F03D1/0641 ,  F03D1/0675 ,  F05B2240/301 ,  F05B2240/32 ,  Y02E10/721 ,  Y10T29/49318 ,  Y10T29/49337

Abstract: A blade for a rotor of a wind turbine is divided into a root region closest to the hub and an airfoil region with a lift generating profile furthest away from the hub and a transition region. A base part of the transition region has an axial induction factor, which without flow altering device deviates at least 5% from a target axial induction factor. A number of first flow altering devices are arranged so as to adjust the aerodynamic properties of a longitudinal segment of the transition region to substantially meet the target axial induction factor.

Abstract translation: 用于风力涡轮机的转子的叶片被分成最靠近轮毂的根部区域和具有离轮毂最远的升力产生轮廓的翼型区域和过渡区域。 过渡区域的基本部分具有轴向感应系数，其没有流动改变装置偏离目标轴向感应系数至少5％。 多个第一流动改变装置被布置成调节过渡区域的纵向段的空气动力特性以基本上满足目标轴向感应系数。

公开(公告)号：US08834130B2

公开(公告)日：2014-09-16

申请号：US12935424

申请日：2009-04-02

Applicant: Peter Fuglsang ,  Stefano Bove

Inventor： Peter Fuglsang ,  Stefano Bove

IPC: F03B3/12 ,  F03D1/06

CPC classification number: F03D1/0675 ,  F05B2230/80 ,  F05B2240/301 ,  F05B2240/31 ,  F05B2240/40 ,  Y02E10/721 ,  Y02P70/523 ,  Y10T29/4932

Abstract: A blade for a rotor of a wind turbine having a substantially horizontal rotor shaft, the rotor comprising a hub, from which the blade extends substantially in a radial direction when mounted to the hub. The blade comprises a main blade part having a profiled contour comprising a pressure side and a suction side as well as a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge. The profiled contour generates a lift when being impacted by an incident airflow. The profiled contour is divided in the radial direction into a root region with a substantially circular or elliptical profile closest to the hub, the substantially circular or elliptical profile having a diameter, an airfoil region with a lift generating profile furthest away from the hub, and a transition region between the root region and the airfoil region. The profile of the transition region gradually changes in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region. The blade further comprises a first auxiliary airfoil having a first pressure side and a first suction side as well as a first chord extending between a first leading edge and a first trailing edge. The first chord has a length that is 75% or less of the diameter of the substantially circular or elliptical profile in the root region and the first auxiliary airfoil is arranged so that it extends in the radial direction along at least a part of the root region of the main blade part with a distance there between.

Abstract translation: 一种用于具有基本上水平的转子轴的风力涡轮机的转子的叶片，所述转子包括毂，当安装到所述毂时，所述叶片从所述叶片基本上沿径向方向延伸。 叶片包括主叶片部分，其具有包括压力侧和吸力侧的轮廓轮廓，以及前缘和具有在前缘和后缘之间延伸的弦的后缘。 异型轮廓在被入射气流撞击时产生电梯。 成型轮廓沿径向方向分成具有最靠近轮毂的大致圆形或椭圆形轮廓的根部区域，基本圆形或椭圆形轮廓具有直径，具有最远离轮毂的升力产生轮廓的翼型区域，以及 在根部区域和翼型区域之间的过渡区域。 过渡区域的轮廓在径向方向上从根部区域的圆形或椭圆形轮廓逐渐变化到翼型区域的升力产生轮廓。 叶片还包括具有第一压力侧和第一吸力侧的第一辅助翼型以及在第一前缘和第一后缘之间延伸的第一弦。 第一弦具有在根部区域中基本上圆形或椭圆形轮廓的直径的75％或更小的长度，并且第一辅助翼型被布置成使得其沿着根部区域的至少一部分在径向方向上延伸 的主叶片部分之间有一段距离。

公开(公告)号：US08579594B2

公开(公告)日：2013-11-12

申请号：US12733362

申请日：2008-08-29

Applicant: Peter Fuglsang ,  Stefano Bove

Inventor： Peter Fuglsang ,  Stefano Bove

IPC: B63H1/28 ,  B64C11/16 ,  F01D5/14

CPC classification number: F01D5/145 ,  B64C2230/26 ,  B64C2230/28 ,  F03D1/0675 ,  F05B2240/122 ,  F05B2240/30 ,  F05D2240/127 ,  F05D2240/30 ,  Y02E10/721 ,  Y02T50/166 ,  Y02T50/673

Abstract: A wind turbine blade having a longitudinal direction with a root end and a tip end as well as a chord extending in a transverse direction between a leading edge and a trailing edge is described. The blade comprises a flow control surface with a suction side and a pressure side. A number of boundary layer control means is formed in the flow control surface. The boundary layer control means include a channel submerged in the flow control surface with a first end facing towards the leading edge and a second end facing towards the trailing edge of the blade. The channel comprises: a bottom surface extending from the first end to the second end, a first sidewall extending between the flow control surface and the bottom surface and extending between the first end and the second end, the first sidewall forming a first sidewall edge between the first side wall and the flow control surface, and a second sidewall extending between the flow control surface and the bottom surface and extending between the first end and the second end, the second sidewall forming a second sidewall edge between the second side wall and the flow control surface. The channel at the first end comprises a first flow accelerating channel zone adapted for accelerating a flow, and at the second end comprises a second channel zone, where the first sidewall and the second sidewall are diverging towards the trailing edge of the blade.

Abstract translation: 描述了具有根端和尖端的纵向方向的风力涡轮机叶片以及在前缘和后缘之间沿横向方向延伸的弦线。 叶片包括具有吸力侧和压力侧的流动控制表面。 在流量控制面上形成有多个边界层控制装置。 边界层控制装置包括浸没在流量控制表面中的通道，其具有面向前缘的第一端和面向叶片后缘的第二端。 所述通道包括：从所述第一端延伸到所述第二端的底表面，在所述流动控制表面和所述底部表面之间延伸并在所述第一端和所述第二端之间延伸的第一侧壁，所述第一侧壁在第一侧壁之间形成第一侧壁边缘， 所述第一侧壁和所述流动控制表面以及在所述流动控制表面和所述底部表面之间延伸并在所述第一端和所述第二端之间延伸的第二侧壁，所述第二侧壁在所述第二侧壁和所述第二侧壁之间形成第二侧壁边缘， 流量控制面。 第一端处的通道包括适于加速流动的第一流动加速通道区域，并且在第二端部包括第二通道区域，其中第一侧壁和第二侧壁朝向叶片的后缘发散。

公开(公告)号：US20130115098A1

公开(公告)日：2013-05-09

申请号：US13810049

申请日：2010-07-16

Applicant: Jesper Madsen ,  Christian Frank Andersen ,  Peter Fuglsang

Inventor： Jesper Madsen ,  Christian Frank Andersen ,  Peter Fuglsang

IPC: F03D1/06

CPC classification number: F03D1/0633 ,  F03D1/0641 ,  F05B2240/301 ,  F05B2250/62 ,  F05B2250/71 ,  Y02E10/721

Abstract: A blade (10) for a rotor of a wind turbine having a profiled contour divided into: a root region (30), an airfoil region (34), and a transition region (32) between the root region (30) and the airfoil region (34). A shoulder (40) is located at the boundary between the transition region (32) and the airfoil region (34). The blade's profiled contour comprises a local relative thickness defined as the local ratio between a maximum profile thickness (t) and the chord length (c). The ratio between the shoulder width (W) and the blade length (L) being less than or equal to 0.075, and the relative thickness (t/c) in a blade length interval of 0-0.8L is at least 22%.

Abstract translation: 一种用于风力涡轮机转子的叶片（10），其具有轮廓轮廓，分为：根部区域（30），翼型区域（34）和根部区域（30）和翼型件之间的过渡区域（32） 区域（34）。 肩部（40）位于过渡区域（32）和翼型区域（34）之间的边界处。 叶片的轮廓轮廓包括局部相对厚度，其定义为最大轮廓厚度（t）和弦长（c）之间的局部比。 肩宽（W）和叶片长度（L）之间的比率小于或等于0.075，叶片长度间隔为0-0.8L的相对厚度（t / c）至少为22％。